Laser augmented turbojet propulsion system

Power plants – Reaction motor – Electric – nuclear – or radiated energy fluid heating means

Reexamination Certificate

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Details

C060S039821, C060S247000

Reexamination Certificate

active

07080504

ABSTRACT:
The invention is a turbojet propulsion system which includes a compressor section, a turbine section coupled by a shaft to the compressor section, a combustion section mounted between the compressor section and the turbine section, and an exhaust duct coupled to the aft end of said turbine section. A fuel delivery system is incorporated for supplying fuel to the combustion section. A laser assembly provides electromagnetic radiation to the combustion section. An electrical generator coupled to the turbine driven shaft powers the laser assembly.

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